EP2353997A3 - Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box - Google Patents

Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box Download PDF

Info

Publication number
EP2353997A3
EP2353997A3 EP11150939.4A EP11150939A EP2353997A3 EP 2353997 A3 EP2353997 A3 EP 2353997A3 EP 11150939 A EP11150939 A EP 11150939A EP 2353997 A3 EP2353997 A3 EP 2353997A3
Authority
EP
European Patent Office
Prior art keywords
box
manufacturing
horizontal tail
boxes
lateral
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP11150939.4A
Other languages
German (de)
French (fr)
Other versions
EP2353997B1 (en
EP2353997A2 (en
Inventor
Antonio De Julián Aguado
Loreto Martínez Fernández
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SL
Original Assignee
Airbus Operations SL
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SL filed Critical Airbus Operations SL
Publication of EP2353997A2 publication Critical patent/EP2353997A2/en
Publication of EP2353997A3 publication Critical patent/EP2353997A3/en
Application granted granted Critical
Publication of EP2353997B1 publication Critical patent/EP2353997B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

Joining arrangement for the lateral boxes (11, 11') of a horizontal tail stabiliser with a central tubular box and manufacturing method for said box. The boxes (11, 11') are joined using an intermediate joining part (31) that comprises a central box (33, 63, 73), upper (35, 35') and lower (37, 37') lateral flaps, fitting plates (A) for the trimming device and fitting plates (B) for the pivoting device, the join being made with rivets between the skins (15, 15'; 17, 17') of the lateral boxes (11, 11') and said flaps (35; 35'; 37; 37'). The method for manufacturing the intermediate joining part (31) comprises steps to: a) Provide preforms suitable for forming said part (31); b) Form and cure the part (31) made from said preforms using an RTM method.
EP11150939.4A 2010-01-15 2011-01-14 Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box Active EP2353997B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201030038A ES2392617B1 (en) 2010-01-15 2010-01-15 JOINT PROVISION OF THE SIDE DRAWERS OF A HORIZONTAL TAIL STABILIZER WITH A TUBULAR CENTRAL DRAWER AND MANUFACTURING PROCEDURE OF SUCH DRAWER.

Publications (3)

Publication Number Publication Date
EP2353997A2 EP2353997A2 (en) 2011-08-10
EP2353997A3 true EP2353997A3 (en) 2014-04-23
EP2353997B1 EP2353997B1 (en) 2019-04-24

Family

ID=43920021

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11150939.4A Active EP2353997B1 (en) 2010-01-15 2011-01-14 Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box

Country Status (4)

Country Link
US (1) US8720824B2 (en)
EP (1) EP2353997B1 (en)
CN (1) CN102126551B (en)
ES (2) ES2392617B1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10118686B2 (en) 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
US9227718B2 (en) * 2013-06-07 2016-01-05 The Boeing Company Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies
EP2832636A1 (en) * 2013-07-30 2015-02-04 Airbus Operations S.L. Rear fuselage section of an aircraft
US9475570B2 (en) 2013-08-23 2016-10-25 The Boeing Company Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies
FR3019522B1 (en) * 2014-04-07 2016-05-20 Airbus Helicopters REMOVABLE SUSTAINABLE ASSEMBLY OF A GIRAVION AND GIRAVION
EP3015361A1 (en) * 2014-10-30 2016-05-04 Airbus Operations, S.L. Central area arrangement for continuous horizontal tail plane torsion box
FR3030443B1 (en) * 2014-12-18 2016-12-09 Airbus Operations Sas METHOD FOR MANUFACTURING A CENTRAL BOAT COMPONENT INTEGRATING AT LEAST ONE INTERMEDIATE LONGERON AND CENTRAL BOAT BOOM THUS OBTAINED
CN104494808B (en) * 2014-12-23 2017-01-04 无锡透平叶片有限公司 A kind of structure being prone to the shaping of titanium alloy forging height muscle
EP3040268A1 (en) * 2014-12-30 2016-07-06 Airbus Operations, S.L. Stringer stiffened aircraft composite structures
US9919791B2 (en) * 2015-04-15 2018-03-20 Gulfstream Aerospace Corporation Stiffening structures, wing structures, and methods for manufacturing stiffening structures
CA3020777A1 (en) * 2016-04-11 2017-10-19 Noon Home, Inc. Intelligent lighting control bulb detection apparatuses, systems, and methods
US10479471B2 (en) * 2016-11-30 2019-11-19 The Boeing Company Fuselage skin panel connection system and method for connecting skin panels
CN108100230A (en) * 2017-12-01 2018-06-01 中国直升机设计研究所 A kind of helicopter horizontal tail wing box
US11932398B2 (en) * 2020-08-24 2024-03-19 The Boeing Company Horizontal stabilizer assembly for an aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4662587A (en) * 1981-09-30 1987-05-05 The Boeing Company Composite for aircraft wing and method of making
EP1070661A2 (en) * 1999-07-19 2001-01-24 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
US20050236524A1 (en) * 2004-04-27 2005-10-27 The Boeing Company Airfoil box and associated method
EP1918193A1 (en) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrated composite skin for aircraft mid-box lifting surfaces
US20090159742A1 (en) * 2007-12-21 2009-06-25 Gonzalo Ramirez Blanco Lifting structure for aircraft
US20090321575A1 (en) * 2008-06-27 2009-12-31 Airbus Espana S.L. Structure of an aircraft aerofoil

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1765791A (en) * 1927-01-29 1930-06-24 Fokker Aircraft Corp Method and means for constructing airplane wings, fuselages, and other structures
US2567124A (en) * 1946-05-10 1951-09-04 Curtiss Wright Corp Airfoil construction
US3779487A (en) * 1971-04-19 1973-12-18 L Ashton Light weight contoured load carrying structure
US4051289A (en) * 1976-04-12 1977-09-27 General Electric Company Composite airfoil construction
US5098037A (en) * 1989-11-06 1992-03-24 The B. F. Goodrich Company Structural airfoil having integral expulsive system
GB2251001B (en) * 1990-12-20 1994-03-23 Rolls Royce Plc Reinforcement preform of knitted fibres
GB9212697D0 (en) * 1992-06-15 1992-07-29 Short Brothers Plc Composite structure manufacture
FR2699449B1 (en) * 1992-12-17 1995-03-24 Eurocopter France Method for manufacturing connections made of composite material of lattice-shaped structures or lattice elements, and lattice obtained by this method.
FR2721000B1 (en) * 1994-06-10 1996-08-23 Eurocopter France Composite rectifier vane, rectifier comprising it, for anti-torque device with faired rotor and stator rectifier, and their manufacturing process.
GB9504372D0 (en) * 1995-03-04 1995-04-26 British Aerospace A composite laminate
US6945727B2 (en) * 2002-07-19 2005-09-20 The Boeing Company Apparatuses and methods for joining structural members, such as composite structural members
ES2315109B1 (en) * 2006-06-30 2010-01-12 Airbus España, S.L. HARDWARE WITH TORSION DRAWER, OF PLASTIC MATERIAL REINFORCED WITH CARBON FIBERS, TO COUPLING A DRIVE / SPINDLE MOTOR ASSEMBLY FOR THE TRIMADO OF A HORIZONTAL STABILIZER OF AN AIRCRAFT.
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing
FR2916417B1 (en) * 2007-05-23 2009-07-24 Airbus France Sas STRUCTURAL AIRCRAFT ELEMENT LOCATED AT THE INTERFACE BETWEEN A WING AND FUSELAGE
ES2335459B1 (en) * 2007-12-21 2011-02-03 Airbus España S.L. OPTIMIZED CONFIGURATION OF AIRCRAFT ENGINES.
US8714485B2 (en) * 2009-12-15 2014-05-06 The Boeing Company Method of fabricating a hat stringer

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4662587A (en) * 1981-09-30 1987-05-05 The Boeing Company Composite for aircraft wing and method of making
EP1070661A2 (en) * 1999-07-19 2001-01-24 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
US20050236524A1 (en) * 2004-04-27 2005-10-27 The Boeing Company Airfoil box and associated method
EP1918193A1 (en) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrated composite skin for aircraft mid-box lifting surfaces
US20090159742A1 (en) * 2007-12-21 2009-06-25 Gonzalo Ramirez Blanco Lifting structure for aircraft
US20090321575A1 (en) * 2008-06-27 2009-12-31 Airbus Espana S.L. Structure of an aircraft aerofoil

Also Published As

Publication number Publication date
ES2392617A1 (en) 2012-12-12
ES2392617B1 (en) 2013-11-21
US8720824B2 (en) 2014-05-13
CN102126551B (en) 2015-10-14
EP2353997B1 (en) 2019-04-24
EP2353997A2 (en) 2011-08-10
ES2738109T3 (en) 2020-01-20
US20110174928A1 (en) 2011-07-21
CN102126551A (en) 2011-07-20

Similar Documents

Publication Publication Date Title
EP2353997A3 (en) Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box
WO2011098785A3 (en) Method of forming an aerodynamic arrangement by joining of segments
EP2962789A3 (en) Additive manufacturing methods and systems with fiber reinforcement
EP3246973A4 (en) Positive-electrode material for lithium-ion secondary battery, method for producing same, and lithium-ion secondary battery
PT2536546T (en) Method for producing a flat semi-finished product from fiber composite material, and the obtained semi-finished product
EP2497596A3 (en) Method of fabricating a component and a component
EP2682340A3 (en) Joining composite fuselage sections along window belts
WO2011137354A3 (en) Delivery proteins
WO2012127038A3 (en) Method for producing a structural component, and structural component
WO2011131746A3 (en) Heterodimeric antibody fc-containing proteins and methods for production thereof
MX353612B (en) Plastic corrugated container with improved fold lines and method and apparatus for making same.
PT2773497T (en) Tubular composite strut having internal stiffening and method for making the same
EP2490313A3 (en) Energy storage system and controlling method thereof
WO2013006563A3 (en) Method and apparatus for a keep-alive push agent
MX2018000450A (en) Method and system for forming packages.
WO2010130687A3 (en) Method for producing an aircraft fuselage and aircraft fuselage
WO2013010805A3 (en) Dc charging station for charging a plurality of energy storage devices
EP2961689A4 (en) Sulfur-carbon composite for lithium-sulfur battery, the method for preparing said composite, and the electrode material and lithium-sulfur battery comprising said composite
WO2010063834A3 (en) Method for manufacturing a reagent container collective and reagent container collective
WO2009156549A3 (en) Structure of an aircraft aerofoil
WO2012028467A8 (en) Air sucking vehicle fuselage component, method for producing an air sucking vehicle fuselage component and a vehicle, especially an aircraft, with an air sucking vehicle fuselage component
EP3130604A4 (en) Anti-il-17 antibodies, method for producing same and method for using same
WO2012062824A3 (en) Method, device, and molding shell for producing a three-dimensional preform in the course of producing fiber-reinforced molded parts
WO2012087656A3 (en) Hollow microspheres and method of making hollow microspheres
EP3780195A4 (en) Method for producing catalyst for air secondary batteries, method for producing air secondary battery, catalyst for air secondary batteries, and air secondary battery

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RIC1 Information provided on ipc code assigned before grant

Ipc: B64C 5/02 20060101ALI20140317BHEP

Ipc: B64C 1/26 20060101AFI20140317BHEP

17P Request for examination filed

Effective date: 20141020

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20171201

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20181119

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1123834

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190515

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602011058258

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190424

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190824

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190724

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190725

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190724

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1123834

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190824

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2738109

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20200120

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602011058258

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

26N No opposition filed

Effective date: 20200127

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20200131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200114

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200114

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20220119

Year of fee payment: 12

Ref country code: DE

Payment date: 20220119

Year of fee payment: 12

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20220119

Year of fee payment: 12

Ref country code: ES

Payment date: 20220325

Year of fee payment: 12

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190424

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602011058258

Country of ref document: DE

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20230114

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230114

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230801

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230131

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20240327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230115